GOE 460 AIRFOIL (goe460-il) Xfoil prediction polar at RE=500,000 Ncrit=5
| Details | Polar file |
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Airfoil: GOE 460 AIRFOIL (goe460-il) Reynolds number: 500,000 Max Cl/Cd: 50.57 at α=9.75° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-goe460-il-500000-n5.txt Download as CSV file: xf-goe460-il-500000-n5.csv |
XFOIL Version 6.96
Calculated polar for: GOE 460 AIRFOIL
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.500 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.750 -1.0716 0.09212 0.08702 -0.0526 1.0000 0.0465
-19.500 -1.0783 0.08816 0.08300 -0.0539 1.0000 0.0471
-19.250 -1.0838 0.08439 0.07915 -0.0551 1.0000 0.0478
-19.000 -1.0876 0.08089 0.07557 -0.0561 1.0000 0.0487
-18.750 -1.0905 0.07755 0.07215 -0.0570 1.0000 0.0493
-18.500 -1.0944 0.07415 0.06866 -0.0579 1.0000 0.0500
-18.250 -1.1022 0.07032 0.06477 -0.0588 1.0000 0.0507
-18.000 -1.1093 0.06665 0.06105 -0.0595 1.0000 0.0517
-17.750 -1.1138 0.06337 0.05769 -0.0601 1.0000 0.0525
-17.500 -1.1169 0.06032 0.05458 -0.0605 1.0000 0.0535
-17.250 -1.1193 0.05739 0.05159 -0.0608 1.0000 0.0547
-17.000 -1.1199 0.05474 0.04886 -0.0610 1.0000 0.0556
-16.750 -1.1226 0.05193 0.04600 -0.0610 1.0000 0.0569
-16.500 -1.1261 0.04914 0.04316 -0.0609 1.0000 0.0584
-16.250 -1.1271 0.04667 0.04064 -0.0606 1.0000 0.0598
-16.000 -1.1262 0.04445 0.03837 -0.0602 1.0000 0.0614
-15.750 -1.1259 0.04225 0.03613 -0.0597 1.0000 0.0633
-15.500 -1.1260 0.04011 0.03397 -0.0589 1.0000 0.0658
-15.250 -1.1245 0.03818 0.03201 -0.0581 1.0000 0.0688
-15.000 -1.1235 0.03631 0.03015 -0.0570 1.0000 0.0728
-14.750 -1.1213 0.03463 0.02846 -0.0558 1.0000 0.0778
-14.500 -1.1176 0.03314 0.02697 -0.0545 1.0000 0.0832
-14.250 -1.1127 0.03183 0.02565 -0.0531 1.0000 0.0873
-14.000 -1.1082 0.03058 0.02437 -0.0515 1.0000 0.0912
-13.750 -1.1014 0.02955 0.02329 -0.0498 1.0000 0.0942
-13.500 -1.0961 0.02852 0.02223 -0.0479 1.0000 0.0964
-13.250 -1.0938 0.02741 0.02111 -0.0456 1.0000 0.0989
-13.000 -1.0906 0.02646 0.02013 -0.0431 1.0000 0.1015
-12.750 -1.0866 0.02564 0.01928 -0.0405 1.0000 0.1038
-12.500 -1.0718 0.02489 0.01847 -0.0398 0.9994 0.1059
-12.250 -1.0512 0.02381 0.01739 -0.0406 0.9975 0.1090
-12.000 -1.0296 0.02285 0.01642 -0.0413 0.9949 0.1122
-11.750 -1.0069 0.02202 0.01556 -0.0420 0.9914 0.1152
-11.500 -0.9840 0.02126 0.01477 -0.0425 0.9878 0.1180
-11.250 -0.9614 0.02036 0.01388 -0.0433 0.9838 0.1223
-11.000 -0.9357 0.01958 0.01310 -0.0444 0.9806 0.1272
-10.750 -0.9128 0.01883 0.01236 -0.0449 0.9769 0.1327
-10.500 -0.8916 0.01809 0.01165 -0.0449 0.9712 0.1404
-10.250 -0.8674 0.01731 0.01095 -0.0456 0.9671 0.1542
-10.000 -0.8409 0.01669 0.01039 -0.0465 0.9632 0.1689
-9.750 -0.8180 0.01619 0.00992 -0.0464 0.9568 0.1778
-9.500 -0.7875 0.01577 0.00948 -0.0477 0.9531 0.1846
-9.250 -0.7545 0.01531 0.00904 -0.0496 0.9502 0.1914
-9.000 -0.7244 0.01498 0.00869 -0.0507 0.9448 0.1974
-8.750 -0.6928 0.01458 0.00827 -0.0522 0.9387 0.2021
-8.500 -0.6577 0.01416 0.00786 -0.0544 0.9338 0.2072
-8.250 -0.6291 0.01385 0.00753 -0.0551 0.9250 0.2119
-8.000 -0.5947 0.01356 0.00720 -0.0569 0.9172 0.2161
-7.750 -0.5696 0.01319 0.00683 -0.0570 0.9060 0.2218
-7.500 -0.5402 0.01288 0.00649 -0.0578 0.8948 0.2264
-7.250 -0.5131 0.01264 0.00620 -0.0580 0.8818 0.2304
-7.000 -0.4881 0.01245 0.00594 -0.0577 0.8684 0.2333
-6.750 -0.4670 0.01220 0.00565 -0.0568 0.8553 0.2379
-6.500 -0.4473 0.01197 0.00539 -0.0554 0.8435 0.2438
-6.250 -0.4278 0.01179 0.00518 -0.0540 0.8324 0.2486
-5.750 -0.3919 0.01142 0.00476 -0.0504 0.8113 0.2608
-5.500 -0.3733 0.01126 0.00457 -0.0487 0.8014 0.2683
-5.250 -0.3578 0.01104 0.00438 -0.0464 0.7909 0.2781
-5.000 -0.3411 0.01086 0.00419 -0.0443 0.7811 0.2896
-4.500 -0.3116 0.01045 0.00385 -0.0393 0.7570 0.3220
-4.250 -0.2968 0.01029 0.00370 -0.0367 0.7431 0.3369
-4.000 -0.2817 0.01015 0.00357 -0.0342 0.7266 0.3505
-3.750 -0.2660 0.01004 0.00345 -0.0317 0.7110 0.3628
-3.500 -0.2501 0.00997 0.00334 -0.0292 0.6945 0.3751
-3.250 -0.2357 0.00992 0.00326 -0.0265 0.6770 0.3857
-3.000 -0.2198 0.00992 0.00320 -0.0240 0.6608 0.3955
-2.750 -0.2060 0.00990 0.00315 -0.0210 0.6461 0.4058
-2.500 -0.1884 0.00989 0.00311 -0.0189 0.6334 0.4150
-2.250 -0.1716 0.00985 0.00307 -0.0166 0.6224 0.4261
-2.000 -0.1541 0.00982 0.00303 -0.0144 0.6103 0.4379
-1.750 -0.1356 0.00979 0.00300 -0.0125 0.5986 0.4508
-1.500 -0.1189 0.00977 0.00298 -0.0102 0.5869 0.4633
-1.250 -0.0984 0.00973 0.00295 -0.0086 0.5776 0.4738
-1.000 -0.0795 0.00971 0.00294 -0.0067 0.5684 0.4853
-0.750 -0.0591 0.00969 0.00292 -0.0052 0.5582 0.4947
-0.500 -0.0399 0.00970 0.00291 -0.0033 0.5468 0.5046
-0.250 -0.0195 0.00969 0.00291 -0.0018 0.5352 0.5136
0.000 0.0000 0.00970 0.00291 0.0000 0.5243 0.5242
0.250 0.0195 0.00969 0.00291 0.0018 0.5136 0.5352
0.500 0.0400 0.00970 0.00291 0.0033 0.5046 0.5467
0.750 0.0592 0.00969 0.00292 0.0052 0.4949 0.5585
1.000 0.0797 0.00971 0.00294 0.0067 0.4858 0.5684
1.250 0.0989 0.00972 0.00295 0.0085 0.4747 0.5776
1.500 0.1189 0.00977 0.00298 0.0102 0.4631 0.5868
1.750 0.1357 0.00979 0.00300 0.0125 0.4505 0.5981
2.000 0.1541 0.00982 0.00303 0.0145 0.4375 0.6102
2.250 0.1716 0.00985 0.00307 0.0166 0.4263 0.6227
2.500 0.1886 0.00988 0.00311 0.0188 0.4154 0.6339
3.000 0.2199 0.00992 0.00320 0.0239 0.3957 0.6610
3.250 0.2355 0.00992 0.00326 0.0265 0.3860 0.6784
3.500 0.2502 0.00997 0.00334 0.0292 0.3751 0.6944
3.750 0.2661 0.01004 0.00345 0.0317 0.3629 0.7112
4.000 0.2816 0.01014 0.00357 0.0342 0.3508 0.7279
4.250 0.2971 0.01029 0.00370 0.0367 0.3373 0.7427
4.500 0.3116 0.01045 0.00385 0.0393 0.3220 0.7575
5.000 0.3414 0.01085 0.00419 0.0443 0.2898 0.7809
5.250 0.3577 0.01104 0.00438 0.0464 0.2777 0.7909
5.500 0.3733 0.01126 0.00457 0.0487 0.2679 0.8014
5.750 0.3920 0.01141 0.00476 0.0504 0.2609 0.8115
6.250 0.4280 0.01179 0.00518 0.0539 0.2487 0.8325
6.500 0.4473 0.01197 0.00539 0.0554 0.2434 0.8432
6.750 0.4673 0.01219 0.00565 0.0567 0.2381 0.8557
7.000 0.4884 0.01245 0.00594 0.0577 0.2332 0.8683
7.250 0.5132 0.01264 0.00620 0.0580 0.2303 0.8816
7.500 0.5404 0.01288 0.00649 0.0578 0.2262 0.8947
7.750 0.5698 0.01319 0.00683 0.0570 0.2214 0.9062
8.000 0.5952 0.01357 0.00720 0.0568 0.2159 0.9174
8.250 0.6297 0.01385 0.00753 0.0550 0.2118 0.9253
8.500 0.6580 0.01416 0.00785 0.0543 0.2072 0.9338
8.750 0.6933 0.01457 0.00826 0.0521 0.2022 0.9387
9.000 0.7246 0.01498 0.00868 0.0507 0.1977 0.9446
9.250 0.7551 0.01529 0.00903 0.0495 0.1927 0.9502
9.500 0.7880 0.01577 0.00948 0.0476 0.1844 0.9531
9.750 0.8188 0.01619 0.00991 0.0463 0.1776 0.9570
10.000 0.8411 0.01670 0.01039 0.0464 0.1679 0.9635
10.250 0.8685 0.01728 0.01093 0.0454 0.1552 0.9671
10.500 0.8926 0.01808 0.01164 0.0447 0.1404 0.9713
10.750 0.9135 0.01881 0.01234 0.0448 0.1326 0.9769
11.000 0.9367 0.01957 0.01308 0.0442 0.1271 0.9807
11.250 0.9628 0.02033 0.01385 0.0431 0.1225 0.9840
11.500 0.9854 0.02123 0.01474 0.0423 0.1181 0.9880
11.750 1.0081 0.02200 0.01554 0.0418 0.1150 0.9915
12.000 1.0309 0.02283 0.01640 0.0411 0.1121 0.9951
12.250 1.0528 0.02378 0.01735 0.0403 0.1090 0.9977
12.500 1.0733 0.02487 0.01845 0.0395 0.1060 0.9995
12.750 1.0871 0.02560 0.01924 0.0405 0.1039 1.0000
13.000 1.0911 0.02641 0.02009 0.0431 0.1015 1.0000
13.250 1.0944 0.02737 0.02106 0.0455 0.0988 1.0000
13.500 1.0970 0.02846 0.02217 0.0478 0.0964 1.0000
13.750 1.1025 0.02948 0.02322 0.0497 0.0940 1.0000
14.000 1.1091 0.03052 0.02431 0.0514 0.0908 1.0000
14.250 1.1134 0.03180 0.02560 0.0530 0.0870 1.0000
14.500 1.1188 0.03308 0.02691 0.0544 0.0832 1.0000
14.750 1.1225 0.03457 0.02839 0.0557 0.0774 1.0000
15.000 1.1246 0.03626 0.03009 0.0569 0.0723 1.0000
15.250 1.1257 0.03813 0.03196 0.0579 0.0683 1.0000
15.500 1.1276 0.04004 0.03389 0.0588 0.0656 1.0000
15.750 1.1271 0.04222 0.03610 0.0595 0.0630 1.0000
16.000 1.1280 0.04438 0.03829 0.0600 0.0612 1.0000
16.250 1.1291 0.04658 0.04055 0.0604 0.0598 1.0000
16.500 1.1281 0.04906 0.04307 0.0607 0.0582 1.0000
16.750 1.1250 0.05182 0.04588 0.0608 0.0568 1.0000
17.000 1.1224 0.05462 0.04874 0.0607 0.0555 1.0000
17.250 1.1218 0.05730 0.05149 0.0605 0.0546 1.0000
17.500 1.1192 0.06025 0.05450 0.0602 0.0534 1.0000
17.750 1.1161 0.06330 0.05763 0.0598 0.0524 1.0000
18.000 1.1116 0.06660 0.06098 0.0592 0.0515 1.0000
18.250 1.1049 0.07024 0.06468 0.0585 0.0506 1.0000
18.500 1.0966 0.07414 0.06864 0.0575 0.0498 1.0000
18.750 1.0945 0.07733 0.07192 0.0567 0.0493 1.0000
19.000 1.0909 0.08076 0.07544 0.0558 0.0486 1.0000
19.250 1.0875 0.08421 0.07896 0.0548 0.0479 1.0000
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